@inproceedings{oai:jaxa.repo.nii.ac.jp:00038666,
 author = {安田, 進 and 内田, 英樹 and Yasuda, Susumu and Uchida, Hideki},
 book = {第58回宇宙科学技術連合講演会講演集, Proceedings of 58th Space Sciences and Technology Conference},
 month = {Nov},
 note = {第58回宇宙科学技術連合講演会（2014年11月12日-14日. 長崎ブリックホール), 長崎市, 長崎県, The infrared space telescope SPICA (Space Infrared Telescope for Cosmology and Astrophysics) is a next-generation astronomical mission in JAXA, which has a 3m-class and 6K cryogenically-cooled space telescope. The connecting part between the mission module and the bus module has low thermal conductivity to reduce heat penetration to the telescope module and low vibration transmissibility to reduce the micro-vibration transferred to the telescope module. As the stiffness of the connecting part is quite low, some kind of damping mechanism are demanded to suppress natural frequency of the connecting part, but dampers utilizes viscoelastic material or oil are not applicable as the operating temperature of the connecting part is supposed to be around 30 K. In this paper, we studied applicability of eddy current damper for the connecting part of SPICA., 資料番号: AC1500025000, レポート番号: JSASS-2014-4143},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {極低温用渦電流ダンパ},
 year = {2014}
}